3D inverse method for turbomachine blading with splitter blades

X. Qiu, T. Dang

Research output: Chapter in Book/Entry/PoemConference contribution

6 Scopus citations

Abstract

The use of a full 3D and viscous inverse method for turbomachine blading with splitter blades is demonstrated by carrying out a design modification of a transonic axial stator blade row with splitter blades. In this design modification study, the goal is to improve the aerodynamics of the full blade and the splitter blade, including weakening of shock wave and control of flow incidence. The improved blade design is "validated" using a well-known 3D Navier-Stokes analysis solver.

Original languageEnglish (US)
Title of host publicationAircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery
PublisherAmerican Society of Mechanical Engineers (ASME)
ISBN (Electronic)9780791878545, 9780791878545
DOIs
StatePublished - 2000
EventASME Turbo Expo 2000: Power for Land, Sea, and Air, GT 2000 - Munich, Germany
Duration: May 8 2000May 11 2000

Publication series

NameProceedings of the ASME Turbo Expo
Volume1

Other

OtherASME Turbo Expo 2000: Power for Land, Sea, and Air, GT 2000
Country/TerritoryGermany
CityMunich
Period5/8/005/11/00

ASJC Scopus subject areas

  • General Engineering

Fingerprint

Dive into the research topics of '3D inverse method for turbomachine blading with splitter blades'. Together they form a unique fingerprint.

Cite this